AFRP Kevlar 49/Epoxy Unidirectional
VerifiedcompositeAramid fiber-reinforced plastic (AFRP) combining DuPont Kevlar 49 aramid fibers in a unidirectional 0° orientation with epoxy matrix, processed as prepreg and cured at 120°C. This material is engineered for applications demanding high specific strength, excellent impact resistance, and low density in a fiber-dominated, load-aligned configuration. Industries rely on it for ballistic protection, aerospace structures, and high-performance sporting goods where weight savings and damage tolerance outweigh the cost premium relative to glass or carbon fiber composites.
Compliance & Regulations
Fiber Direction
Ply Schedule
Laminate Code
[0]T
Fiber angles relative to the 0° reference direction (red arrow in 3D view). 0° = longitudinal, 90° = transverse, ±45° = shear paths.
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 1.800 | - | — | ||
Poisson's Ratio(ν) | 0.3400 | - | — | ||
Ultimate Tensile Strength(σUTS) | 1.380 | GPa | — | ||
Young's Modulus(E) | 76.00 | GPa | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Maximum Service Temperature(Tmax) | 423 | K | — | ||
Coefficient of Thermal Expansion(α (CTE)) | -0.00000400 | 1/K | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 1.380 | kg/m³ | — |